[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 24th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
270/16:51:47
699 -0
9 1
4 1
4
N/A -0
9 0
0 220
7
000/00:03:35
398 -0
6 0
0 215
8
274/01:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
6
277/10:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2017/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4249537
99 A = 6777125
31 meter
Y = -9962
41 meter E =
0012067
Z = -5289518
02 I = 51
24311
XDOT = 200
378677 Wp = 76
03375
YDOT = -7656
130859 meter/sec RA = 272
36394 deg
ZDOT = -143
978680 TA = 192
57004
MA = 192
60016
Ha = 220
109 n
mi
Hp = 215
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13942053
78 X = -4223416
61
Y = -32685
07 feet Y = -57338
29 meter
Z = -17354061
75 Z = -5310097
71
XDOT = 657
410357 XDOT = 286
676062
YDOT = -25118
539563 feet/sec YDOT = -7653
407589 meter/sec
ZDOT = -472
370998 ZDOT = -142
794671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13827390
67 X = 4214588
68
Y = -128516
84 feet Y = -39171
93 meter
Z = -17445117
99 Z = -5317271
96
XDOT = -374
403124 XDOT = -114
118072
YDOT = 24116
299335 feet/sec YDOT = 7350
648037 meter/sec
ZDOT = -465
991402 ZDOT = -142
034179
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17265
51632839
00016717 00000-0 10270-3 0 9005
2 25544 51
6384 273
1329 0004097 309
7753 50
3038 15
54210030 36885
Satellite: ISS
Catalog Number: 25544
Epoch time: 17265
51632839 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 273
1329 deg
Eccentricity:
0004097
Arg of perigee: 309
7753 deg
Mean anomaly: 50
3038 deg
Mean motion: 15
54210030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 304
Coasting Arc #2 (Orbit 3703)
---------------------------------------
Vector Time (GMT): 2017/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4134177
77 A = 6778142
39 meter
Y = 1867549
42 meter E =
0006171
Z = 5036586
77 I = 51
24591
XDOT = -1113
061802 Wp = 14
44401
YDOT = 7367
559447 meter/sec RA = 267
33521 deg
ZDOT = -1811
873425 TA = 93
22839
MA = 93
15778
Ha = 220
112 n
mi
Hp = 215
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13563575
37 X = 4088521
51
Y = 6127130
65 feet Y = 1913525
94 meter
Z = 16524234
80 Z = 5056558
45
XDOT = -3651
777565 XDOT = -1186
563786
YDOT = 24171
782963 feet/sec YDOT = 7354
701240 meter/sec
ZDOT = -5944
466619 ZDOT = -1817
459805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13626750
16 X = -4153433
45
Y = -5736278
45 feet Y = -1748417
67 meter
Z = 16612327
72 Z = 5063437
49
XDOT = 2492
919993 XDOT = 759
842014
YDOT = -23272
098919 feet/sec YDOT = -7093
335750 meter/sec
ZDOT = -5970
270599 ZDOT = -1819
738479
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17266
54509468
00016717 00000-0 10270-3 0 9011
2 25544 51
6379 268
0029 0004135 314
2890 45
7923 15
54234212 37043
Satellite: ISS
Catalog Number: 25544
Epoch time: 17266
54509468 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 268
0029 deg
Eccentricity:
0004135
Arg of perigee: 314
2890 deg
Mean anomaly: 45
7923 deg
Mean motion: 15
54234212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3704
Checksum: 308
Coasting Arc #3 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2017/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3919878
01 A = 6781329
16 meter
Y = -3548538
49 meter E =
0005133
Z = -4250283
94 I = 51
25940
XDOT = 2009
224992 Wp = 86
36522
YDOT = -6481
268820 meter/sec RA = 262
31402 deg
ZDOT = 3562
195976 TA = 220
19414
MA = 220
23211
Ha = 220
348 n
mi
Hp = 215
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12860492
15 X = -3859259
90
Y = -11642186
66 feet Y = -3592034
75 meter
Z = -13944501
12 Z = -4269178
14
XDOT = 6591
945512 XDOT = 2064
247302
YDOT = -21264
005316 feet/sec YDOT = -6458
492277 meter/sec
ZDOT = 11686
994673 ZDOT = 3572
090614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13292490
27 X = 4051551
04
Y = 11041666
86 feet Y = 3365500
06 meter
Z = -14027586
22 Z = -4275608
28
XDOT = -4721
774774 XDOT = -1439
196951
YDOT = 20571
752000 feet/sec YDOT = 6270
270010 meter/sec
ZDOT = 11731
722013 ZDOT = 3575
828870
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17267
50955981
00016717 00000-0 10270-3 0 9024
2 25544 51
6384 263
1947 0004179 320
1639 39
9206 15
54214939 37198
Satellite: ISS
Catalog Number: 25544
Epoch time: 17267
50955981 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 263
1947 deg
Eccentricity:
0004179
Arg of perigee: 320
1639 deg
Mean anomaly: 39
9206 deg
Mean motion: 15
54214939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3719
Checksum: 336
Coasting Arc #4 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2017/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3562656
27 A = 6785116
22 meter
Y = 4942358
76 meter E =
0010609
Z = 2979720
00 I = 51
27668
XDOT = -2913
901198 Wp = 79
61883
YDOT = 5089
148820 meter/sec RA = 257
30268 deg
ZDOT = -4940
312250 TA = 66
10827
MA = 65
99715
Ha = 220
426 n
mi
Hp = 215
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11688504
82 X = 3492650
50
Y = 16215087
80 feet Y = 4981807
66 meter
Z = 9775984
26 Z = 2996856
02
XDOT = -9560
043300 XDOT = -2946
594915
YDOT = 16696
682481 feet/sec YDOT = 5056
380340 meter/sec
ZDOT = -16208
373525 ZDOT = -4954
547134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12627685
08 X = -3848918
41
Y = -15447250
26 feet Y = -4708321
88 meter
Z = 9851097
13 Z = 3002614
41
XDOT = 7250
894257 XDOT = 2210
072569
YDOT = -16339
657461 feet/sec YDOT = -4980
327594 meter/sec
ZDOT = -16272
097487 ZDOT = -4959
735314
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17268
53831863
00016717 00000-0 10270-3 0 9031
2 25544 51
6372 258
0650 0004374 323
4266 36
6588 15
54263356 37350
Satellite: ISS
Catalog Number: 25544
Epoch time: 17268
53831863 = yrday
fracday
Element set: 903
Inclination: 51
6372 deg
RA of node: 258
0650 deg
Eccentricity:
0004374
Arg of perigee: 323
4266 deg
Mean anomaly: 36
6588 deg
Mean motion: 15
54263356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3735
Checksum: 325
Coasting Arc #5 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2017/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3060762
03 A = 6788082
86 meter
Y = -5886423
10 meter E =
0010638
Z = -1405878
38 I = 51
29473
XDOT = 3787
555272 Wp = 16
37376
YDOT = -3342
830189 meter/sec RA = 252
30290 deg
ZDOT = 5771
213425 TA = 328
22133
MA = 328
28548
Ha = 220
484 n
mi
Hp = 215
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10041870
17 X = -2987881
84
Y = -19312411
73 feet Y = -5920243
24 meter
Z = -4612461
87 Z = -1420569
30
XDOT = 12426
362442 XDOT = 3796
620122
YDOT = -10967
290646 feet/sec YDOT = -3300
424014 meter/sec
ZDOT = 18934
427247 ZDOT = 5789
634702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11533272
68 X = 3515341
51
Y = 18444401
39 feet Y = 5621853
54 meter
Z = -4676631
97 Z = -1425437
42
XDOT = -10034
465858 XDOT = -3058
505194
YDOT = 11079
222923 feet/sec YDOT = 3376
947147 meter/sec
ZDOT = 19016
423317 ZDOT = 5796
205827
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17269
50277888
00016717 00000-0 10270-3 0 9041
2 25544 51
6372 253
2571 0004120 327
4101 32
6797 15
54260194 37502
Satellite: ISS
Catalog Number: 25544
Epoch time: 17269
50277888 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 253
2571 deg
Eccentricity:
0004120
Arg of perigee: 327
4101 deg
Mean anomaly: 32
6797 deg
Mean motion: 15
54260194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3750
Checksum: 307
Coasting Arc #6 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2017/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2352884
40 A = 6788887
87 meter
Y = 6355429
48 meter E =
0007272
Z = -350889
56 I = 51
30922
XDOT = -4605
617673 Wp = 128
64745
YDOT = 1380
326800 meter/sec RA = 247
30804 deg
ZDOT = -5970
387429 TA = 55
15097
MA = 55
08261
Ha = 220
698 n
mi
Hp = 215
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7719437
00 X = 2283345
89
Y = 20851146
60 feet Y = 6381352
20 meter
Z = -1151212
45 Z = -339629
22
XDOT = -15110
294203 XDOT = -4591
709033
YDOT = 4528
631233 feet/sec YDOT = 1328
900971 meter/sec
ZDOT = -19587
885265 ZDOT = -5992
726645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9725323
39 X = -2964278
57
Y = -19997209
41 feet Y = -6095149
43 meter
Z = -1102276
24 Z = -335973
80
XDOT = 13009
815441 XDOT = 3965
391746
YDOT = -5258
644693 feet/sec YDOT = -1602
834903 meter/sec
ZDOT = -19686
943693 ZDOT = -6000
580438
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17270
53153100
00016717 00000-0 10270-3 0 9057
2 25544 51
6381 248
1269 0004368 332
1021 27
9897 15
54262658 37669
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
53153100 = yrday
fracday
Element set: 905
Inclination: 51
6381 deg
RA of node: 248
1269 deg
Eccentricity:
0004368
Arg of perigee: 332
1021 deg
Mean anomaly: 27
9897 deg
Mean motion: 15
54262658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 310
Coasting Arc #7 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/270/16:53:35
398
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2388501
75 A = 6779821
85 meter
Y = 4150588
55 meter E =
0010499
Z = -4808989
24 I = 51
28227
XDOT = -4631
308698 Wp = 49
04985
YDOT = -5565
465384 meter/sec RA = 246
30425 deg
ZDOT = -2500
072476 TA = 196
20505
MA = 196
23865
Ha = 220
682 n
mi
Hp = 215
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7836291
82 X = -2411377
26
Y = 13617416
51 feet Y = 4123750
44 meter
Z = -15777523
75 Z = -4820647
82
XDOT = -15194
582341 XDOT = -4556
585723
YDOT = -18259
400867 feet/sec YDOT = -5616
838217 meter/sec
ZDOT = -8202
337519 ZDOT = -2522
388268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11926045
17 X = -3635058
57
Y = -10147001
94 feet Y = -3092806
19 meter
Z = -15829704
85 Z = -4824894
04
XDOT = 20033
683496 XDOT = 6106
266730
YDOT = -10581
151026 feet/sec YDOT = -3225
134833 meter/sec
ZDOT = -8300
315447 ZDOT = -2529
936148
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17270
72442365
00016717 00000-0 10270-3 0 9063
2 25544 51
6414 247
1666 0004539 317
4594 42
6207 15
54010516 37693
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
72442365 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 247
1666 deg
Eccentricity:
0004539
Arg of perigee: 317
4594 deg
Mean anomaly: 42
6207 deg
Mean motion: 15
54010516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 310
Coasting Arc #8 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2017/271/16:53:35
398
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3319683
37 A = 6777834
89 meter
Y = -2704501
41 meter E =
0002072
Z = 5253936
44 I = 51
28909
XDOT = 4143
264488 Wp = 355
12874
YDOT = 6416
498221 meter/sec RA = 241
28325 deg
ZDOT = 687
078799 TA = 88
28996
MA = 88
26623
Ha = 220
617 n
mi
Hp = 215
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10891349
63 X = 3324157
84
Y = -8873036
14 feet Y = -2667353
06 meter
Z = 17237324
29 Z = 5270073
63
XDOT = 13593
387429 XDOT = 4067
868042
YDOT = 21051
503349 feet/sec YDOT = 6462
409512 meter/sec
ZDOT = 2254
195535 ZDOT = 707
022072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6904657
91 X = 2104539
73
Y = 12132500
13 feet Y = 3697986
04 meter
Z = 17309123
47 Z = 5275820
83
XDOT = -22173
346127 XDOT = -6758
435899
YDOT = 9287
836525 feet/sec YDOT = 2830
932573 meter/sec
ZDOT = 2341
573009 ZDOT = 713
711453
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17271
75334753
00016717 00000-0 10270-3 0 9079
2 25544 51
6406 242
0386 0004534 320
0628 40
0191 15
54018602 37856
Satellite: ISS
Catalog Number: 25544
Epoch time: 17271
75334753 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 242
0386 deg
Eccentricity:
0004534
Arg of perigee: 320
0628 deg
Mean anomaly: 40
0191 deg
Mean motion: 15
54018602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3785
Checksum: 289
Coasting Arc #9 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2017/272/16:53:35
398
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4206611
31 A = 6778137
19 meter
Y = 1186502
85 meter E =
0011319
Z = -5190207
56 I = 51
30684
XDOT = -3375
706478 Wp = 82
64689
YDOT = -6772
449118 meter/sec RA = 236
26140 deg
ZDOT = 1191
428380 TA = 198
82648
MA = 198
86837
Ha = 220
814 n
mi
Hp = 215
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13801218
20 X = -4194354
82
Y = 3892725
88 feet Y = 1139529
79 meter
Z = -17028240
01 Z = -5210612
41
XDOT = -11075
152486 XDOT = -3305
511669
YDOT = -22219
321254 feet/sec YDOT = -6809
805998 meter/sec
ZDOT = 3908
885762 ZDOT = 1175
201151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1744247
92 X = -531646
77
Y = -14124263
76 feet Y = -4305075
60 meter
Z = -17118722
76 Z = -5217786
70
XDOT = 22629
472372 XDOT = 6897
463179
YDOT = -7431
767120 feet/sec YDOT = -2265
202618 meter/sec
ZDOT = 3837
985199 ZDOT = 1169
817889
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17272
71796173
00016717 00000-0 10270-3 0 9085
2 25544 51
6408 237
2314 0004630 323
2098 36
8736 15
54014536 38006
Satellite: ISS
Catalog Number: 25544
Epoch time: 17272
71796173 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 237
2314 deg
Eccentricity:
0004630
Arg of perigee: 323
2098 deg
Mean anomaly: 36
8736 deg
Mean motion: 15
54014536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3800
Checksum: 305
Coasting Arc #10 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2017/273/16:53:35
398
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4974587
02 A = 6780472
47 meter
Y = 322937
04 meter E =
0009001
Z = 4595468
55 I = 51
33455
XDOT = 2317
168381 Wp = 33
64330
YDOT = 6679
674627 meter/sec RA = 231
24401 deg
ZDOT = -2967
572786 TA = 86
12202
MA = 86
01912
Ha = 220
847 n
mi
Hp = 215
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16320823
57 X = 4948283
50
Y = 1059504
72 feet Y = 378419
59 meter
Z = 15076996
56 Z = 4619569
74
XDOT = 7602
258469 XDOT = 2256
717342
YDOT = 21914
943003 feet/sec YDOT = 6705
248525 meter/sec
ZDOT = -9736
131189 ZDOT = -2956
464059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3264355
61 X = -994975
59
Y = 15925092
90 feet Y = 4853968
32 meter
Z = 15183644
36 Z = 4627974
80
XDOT = -21593
952260 XDOT = -6581
836649
YDOT = 4841
988267 feet/sec YDOT = 1475
838024 meter/sec
ZDOT = -9687
856241 ZDOT = -2952
858582
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17273
74687711
00016717 00000-0 10270-3 0 9097
2 25544 51
6413 232
1031 0004781 327
1683 32
9172 15
54050724 38169
Satellite: ISS
Catalog Number: 25544
Epoch time: 17273
74687711 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 232
1031 deg
Eccentricity:
0004781
Arg of perigee: 327
1683 deg
Mean anomaly: 32
9172 deg
Mean motion: 15
54050724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3816
Checksum: 300
Coasting Arc #11 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2017/274/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3509539
28 A = 6789017
29 meter
Y = -5660820
06 meter E =
0014234
Z = 1270133
37 I = 51
36945
XDOT = 4731
437873 Wp = 41
92183
YDOT = -1621
921828 meter/sec RA = 229
43638 deg
ZDOT = 5817
489274 TA = 331
95238
MA = 332
02900
Ha = 220
909 n
mi
Hp = 215
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11514236
47 X = -3452147
35
Y = -18572244
30 feet Y = -5699745
11 meter
Z = 4167104
25 Z = 1253224
97
XDOT = 15523
090136 XDOT = 4720
964356
YDOT = -5321
265840 feet/sec YDOT = -1569
069683 meter/sec
ZDOT = 19086
250900 ZDOT = 5840
447936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20049283
23 X = -6111021
53
Y = -8726062
13 feet Y = -2659703
74 meter
Z = 4093011
05 Z = 1247549
77
XDOT = 9012
323321 XDOT = 2746
956148
YDOT = -11663
819237 feet/sec YDOT = -3555
132103 meter/sec
ZDOT = 19188
105352 ZDOT = 5848
534511
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17274
13272084
00016717 00000-0 10270-3 0 9106
2 25544 51
6406 230
1749 0004189 326
9696 33
1194 15
54010534 38227
Satellite: ISS
Catalog Number: 25544
Epoch time: 17274
13272084 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 230
1749 deg
Eccentricity:
0004189
Arg of perigee: 326
9696 deg
Mean anomaly: 33
1194 deg
Mean motion: 15
54010534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 297
Coasting Arc #12 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2017/275/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2523614
97 A = 6786322
76 meter
Y = 5633535
94 meter E =
0002315
Z = -2822773
03 I = 51
38204
XDOT = -5746
227051 Wp = 57
76591
YDOT = 35
303492 meter/sec RA = 224
44475 deg
ZDOT = -5068
628015 TA = 154
39198
MA = 154
38052
Ha = 220
984 n
mi
Hp = 215
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8279576
68 X = 2474143
42
Y = 18482729
46 feet Y = 5661479
80 meter
Z = -9261066
38 Z = -2810634
82
XDOT = -18852
450956 XDOT = -5721
573739
YDOT = 115
825105 feet/sec YDOT = -28
817455 meter/sec
ZDOT = -16629
357005 ZDOT = -5096
481642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17541406
00 X = 5346620
55
Y = 10170572
14 feet Y = 3099990
39 meter
Z = -9208070
73 Z = -2806619
96
XDOT = -14430
296000 XDOT = -4398
354221
YDOT = 9726
479031 feet/sec YDOT = 2964
630809 meter/sec
ZDOT = -16752
679094 ZDOT = -5106
216588
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17275
09732455
00016717 00000-0 10270-3 0 9116
2 25544 51
6402 225
3678 0004171 329
2212 30
8696 15
54014026 38378
Satellite: ISS
Catalog Number: 25544
Epoch time: 17275
09732455 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 225
3678 deg
Eccentricity:
0004171
Arg of perigee: 329
2212 deg
Mean anomaly: 30
8696 deg
Mean motion: 15
54014026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 298
Coasting Arc #13 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2017/276/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1275351
38 A = 6782519
92 meter
Y = -5263026
05 meter E =
0008560
Z = 4075411
70 I = 51
39451
XDOT = 6501
641182 Wp = 81
11883
YDOT = 1392
233192 meter/sec RA = 219
44521 deg
ZDOT = 3826
964393 TA = 329
18765
MA = 329
23787
Ha = 220
996 n
mi
Hp = 215
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4184223
68 X = -1236200
50
Y = -17267145
82 feet Y = -5277068
47 meter
Z = 13370773
31 Z = 4069312
17
XDOT = 21330
843772 XDOT = 6467
000017
YDOT = 4567
694199 feet/sec YDOT = 1464
745775 meter/sec
ZDOT = 12555
657456 ZDOT = 3858
463214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13722502
88 X = -4182618
88
Y = -11316278
27 feet Y = -3449201
62 meter
Z = 13344451
73 Z = 4067388
89
XDOT = 18958
239440 XDOT = 5778
471381
YDOT = -7997
525041 feet/sec YDOT = -2437
645632 meter/sec
ZDOT = 12694
943645 ZDOT = 3869
418823
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17276
12622944
00016717 00000-0 10270-3 0 9123
2 25544 51
6410 220
2395 0004170 332
3569 27
7361 15
54054963 38532
Satellite: ISS
Catalog Number: 25544
Epoch time: 17276
12622944 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 220
2395 deg
Eccentricity:
0004170
Arg of perigee: 332
3569 deg
Mean anomaly: 27
7361 deg
Mean motion: 15
54054963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 299
Coasting Arc #14 (Orbit 3867)
---------------------------------------
Vector Time (GMT): 2017/277/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -181264
15 A = 6779338
13 meter
Y = 4653509
58 meter E =
0012442
Z = -4937828
10 I = 51
40979
XDOT = -6866
736949 Wp = 53
95419
YDOT = -2591
982789 meter/sec RA = 214
43805 deg
ZDOT = -2187
359637 TA = 194
59565
MA = 194
63160
Ha = 221
179 n
mi
Hp = 215
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -594698
66 X = -209301
70
Y = 15267419
87 feet Y = 4651325
12 meter
Z = -16200223
43 Z = -4938777
37
XDOT = -22528
664532 XDOT = -6826
617138
YDOT = -8503
880542 feet/sec YDOT = -2668
547305 meter/sec
ZDOT = -7176
376761 ZDOT = -2220
618612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8922858
47 X = 2719687
26
Y = 12396562
68 feet Y = 3778472
30 meter
Z = -16205025
33 Z = -4939291
72
XDOT = -22099
191263 XDOT = -6735
833497
YDOT = 6319
315857 feet/sec YDOT = 1926
127473 meter/sec
ZDOT = -7323
315895 ZDOT = -2232
146685
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17277
09082495
00016717 00000-0 10270-3 0 9132
2 25544 51
6414 215
4324 0004323 335
8218 24
2731 15
54015785 38681
Satellite: ISS
Catalog Number: 25544
Epoch time: 17277
09082495 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 215
4324 deg
Eccentricity:
0004323
Arg of perigee: 335
8218 deg
Mean anomaly: 24
2731 deg
Mean motion: 15
54015785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3868
Checksum: 307
Coasting Arc #15 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2017/277/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 643250
70 A = 6780267
84 meter
Y = 4855820
87 meter E =
0011846
Z = -4699430
68 I = 51
42139
XDOT = -6911
616044 Wp = 47
57498
YDOT = -1777
391908 meter/sec RA = 212
52008 deg
ZDOT = -2779
251942 TA = 194
74892
MA = 194
78351
Ha = 221
391 n
mi
Hp = 215
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2110402
56 X = 611731
58
Y = 15931170
83 feet Y = 4862837
26 meter
Z = -15418079
65 Z = -4696383
16
XDOT = -22675
905657 XDOT = -6877
726699
YDOT = -5831
338281 feet/sec YDOT = -1854
493214 meter/sec
ZDOT = -9118
280649 ZDOT = -2812
744222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1222957
49 X = -372757
44
Y = -16036120
67 feet Y = -4887809
58 meter
Z = -15405206
65 Z = -4695506
99
XDOT = 21042
645295 XDOT = 6413
798286
YDOT = 7307
561195 feet/sec YDOT = 2227
344652 meter/sec
ZDOT = -9266
362898 ZDOT = -2824
387411
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17277
47666212
00016717 00000-0 10270-3 0 9140
2 25544 51
6393 213
5108 0004718 342
4226 17
6763 15
54037684 38747
Satellite: ISS
Catalog Number: 25544
Epoch time: 17277
47666212 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 213
5108 deg
Eccentricity:
0004718
Arg of perigee: 342
4226 deg
Mean anomaly: 17
6763 deg
Mean motion: 15
54037684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 321
Coasting Arc #16 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2017/278/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 947907
15 A = 6777865
10 meter
Y = -4205214
89 meter E =
0003205
Z = 5228444
59 I = 51
44190
XDOT = 7071
863300 Wp = 34
65777
YDOT = 2805
429841 meter/sec RA = 207
51091 deg
ZDOT = 976
570030 TA = 45
98519
MA = 45
95879
Ha = 221
351 n
mi
Hp = 215
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3109931
59 X = 969462
92
Y = -13796636
78 feet Y = -4194493
51 meter
Z = 17153689
61 Z = 5233102
23
XDOT = 23201
651248 XDOT = 7035
222868
YDOT = 9204
166146 feet/sec YDOT = 2884
307508 meter/sec
ZDOT = 3203
969915 ZDOT = 1010
834090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3609796
37 X = -1100265
93
Y = 13647776
93 feet Y = 4159842
41 meter
Z = 17174850
31 Z = 5234894
37
XDOT = -21751
205839 XDOT = -6629
767540
YDOT = -9966
179038 feet/sec YDOT = -3037
691371 meter/sec
ZDOT = 3355
352725 ZDOT = 1022
711511
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17278
50555487
00016717 00000-0 10270-3 0 9157
2 25544 51
6393 208
3835 0004782 344
6696 15
4311 15
54068629 38908
Satellite: ISS
Catalog Number: 25544
Epoch time: 17278
50555487 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 208
3835 deg
Eccentricity:
0004782
Arg of perigee: 344
6696 deg
Mean anomaly: 15
4311 deg
Mean motion: 15
54068629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 339
Coasting Arc #17 (Orbit 3904)
---------------------------------------
Vector Time (GMT): 2017/279/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2562384
07 A = 6777848
23 meter
Y = 3459924
16 meter E =
0013759
Z = -5246005
77 I = 51
47153
XDOT = -6709
717501 Wp = 78
05329
YDOT = -3575
492556 meter/sec RA = 202
49914 deg
ZDOT = 924
009086 TA = 200
79022
MA = 200
84623
Ha = 221
527 n
mi
Hp = 214
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8406771
89 X = -2575400
40
Y = 11351457
21 feet Y = 3431196
39 meter
Z = -17211305
02 Z = -5258485
33
XDOT = -22013
508860 XDOT = -6673
725179
YDOT = -11730
618622 feet/sec YDOT = -3650
323837 meter/sec
ZDOT = 3031
525873 ZDOT = 891
502590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8601806
41 X = 2621830
59
Y = -11118344
98 feet Y = -3388871
55 meter
Z = -17267013
24 Z = -5262985
64
XDOT = 20892
202306 XDOT = 6367
943263
YDOT = 11702
906511 feet/sec YDOT = 3567
045905 meter/sec
ZDOT = 2888
010297 ZDOT = 880
265538
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17279
47013848
00016717 00000-0 10270-3 0 9165
2 25544 51
6397 203
5755 0004752 348
6992 11
4053 15
54046953 39052
Satellite: ISS
Catalog Number: 25544
Epoch time: 17279
47013848 = yrday
fracday
Element set: 916
Inclination: 51
6397 deg
RA of node: 203
5755 deg
Eccentricity:
0004752
Arg of perigee: 348
6992 deg
Mean anomaly: 11
4053 deg
Mean motion: 15
54046953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3905
Checksum: 331
Coasting Arc #18 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2017/280/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4095658
41 A = 6780002
29 meter
Y = -2638682
40 meter E =
0010391
Z = 4713288
79 I = 51
51004
XDOT = 5843
175699 Wp = 37
09002
YDOT = 4135
214718 meter/sec RA = 197
49312 deg
ZDOT = -2751
137030 TA = 80
24791
MA = 80
13057
Ha = 221
544 n
mi
Hp = 214
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13437199
51 X = 4101965
09
Y = -8657094
49 feet Y = -2592846
18 meter
Z = 15463545
91 Z = 4733200
29
XDOT = 19170
523946 XDOT = 5809
864329
YDOT = 13566
977421 feet/sec YDOT = 4200
370544 meter/sec
ZDOT = -9026
040126 ZDOT = -2722
833403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13423260
05 X = -4091409
66
Y = 8519035
38 feet Y = 2596601
98 meter
Z = 15552073
61 Z = 4740272
04
XDOT = -18468
410717 XDOT = -5629
171586
YDOT = -12783
283785 feet/sec YDOT = -3896
344898 meter/sec
ZDOT = -8901
196887 ZDOT = -2713
084811
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17280
49901953
00016717 00000-0 10270-3 0 9173
2 25544 51
6402 198
4477 0004807 352
5868 7
5213 15
54057700 39213
Satellite: ISS
Catalog Number: 25544
Epoch time: 17280
49901953 = yrday
fracday
Element set: 917
Inclination: 51
6402 deg
RA of node: 198
4477 deg
Eccentricity:
0004807
Arg of perigee: 352
5868 deg
Mean anomaly: 7
5213 deg
Mean motion: 15
54057700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 320
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